JPS5277910A - Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine - Google Patents

Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine

Info

Publication number
JPS5277910A
JPS5277910A JP14881276A JP14881276A JPS5277910A JP S5277910 A JPS5277910 A JP S5277910A JP 14881276 A JP14881276 A JP 14881276A JP 14881276 A JP14881276 A JP 14881276A JP S5277910 A JPS5277910 A JP S5277910A
Authority
JP
Japan
Prior art keywords
turbine
22shaft
single stage
stage power
equipment connecting
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP14881276A
Other languages
Japanese (ja)
Other versions
JPS5624772B2 (en
Inventor
David J Amos
Taku Ichiyanagi
Taku Ichiryu
Tomotaka Satou
Tomohiko Sato
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US05/643,718 external-priority patent/US3990810A/en
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to JP14881276A priority Critical patent/JPS5277910A/en
Publication of JPS5277910A publication Critical patent/JPS5277910A/en
Publication of JPS5624772B2 publication Critical patent/JPS5624772B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP14881276A 1975-12-23 1976-12-13 Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine Granted JPS5277910A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14881276A JPS5277910A (en) 1975-12-23 1976-12-13 Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/643,718 US3990810A (en) 1975-12-23 1975-12-23 Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine
JP14881276A JPS5277910A (en) 1975-12-23 1976-12-13 Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine

Publications (2)

Publication Number Publication Date
JPS5277910A true JPS5277910A (en) 1977-06-30
JPS5624772B2 JPS5624772B2 (en) 1981-06-08

Family

ID=26478886

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14881276A Granted JPS5277910A (en) 1975-12-23 1976-12-13 Blade equipment connecting 22shaft gas turbine compressor turbine and single stage power turbine

Country Status (1)

Country Link
JP (1) JPS5277910A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11264326A (en) * 1997-12-18 1999-09-28 United Technol Corp <Utc> Seal for variable inlet guide vane of gas turbine engine
JP2002195195A (en) * 2000-11-17 2002-07-10 General Electric Co <Ge> Replaceable variable stator blade for gas turbine
JP2007277669A (en) * 2006-04-10 2007-10-25 Nippon Steel Corp Method for desulfurizing molten iron
JP2010180878A (en) * 2009-02-06 2010-08-19 General Electric Co <Ge> Ceramic matrix composite turbine engine
US9683271B2 (en) 2012-10-10 2017-06-20 Posco Impeller and method of melt-pool processing method using the same
US10077482B2 (en) 2013-08-07 2018-09-18 Posco Molten iron refining method and device thereof
JP2018178897A (en) * 2017-04-17 2018-11-15 三菱日立パワーシステムズ株式会社 Turbine stator vane row
RU2691276C1 (en) * 2018-07-11 2019-06-11 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Adjustable inlet guide vane of gas turbine engine compressor
JP2020037941A (en) * 2018-08-29 2020-03-12 ゼネラル・エレクトリック・カンパニイ Variable nozzle in turbine engine, and related method
RU2767250C1 (en) * 2020-12-14 2022-03-17 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" Adjustable inlet guiding apparatus of the compressor of a gas turbine engine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4826084A (en) * 1971-08-06 1973-04-05
US3887297A (en) * 1974-06-25 1975-06-03 United Aircraft Corp Variable leading edge stator vane assembly

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4826084A (en) * 1971-08-06 1973-04-05
US3887297A (en) * 1974-06-25 1975-06-03 United Aircraft Corp Variable leading edge stator vane assembly

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11264326A (en) * 1997-12-18 1999-09-28 United Technol Corp <Utc> Seal for variable inlet guide vane of gas turbine engine
JP2002195195A (en) * 2000-11-17 2002-07-10 General Electric Co <Ge> Replaceable variable stator blade for gas turbine
JP2007277669A (en) * 2006-04-10 2007-10-25 Nippon Steel Corp Method for desulfurizing molten iron
JP2010180878A (en) * 2009-02-06 2010-08-19 General Electric Co <Ge> Ceramic matrix composite turbine engine
US9683271B2 (en) 2012-10-10 2017-06-20 Posco Impeller and method of melt-pool processing method using the same
US10077482B2 (en) 2013-08-07 2018-09-18 Posco Molten iron refining method and device thereof
JP2018178897A (en) * 2017-04-17 2018-11-15 三菱日立パワーシステムズ株式会社 Turbine stator vane row
RU2691276C1 (en) * 2018-07-11 2019-06-11 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Adjustable inlet guide vane of gas turbine engine compressor
JP2020037941A (en) * 2018-08-29 2020-03-12 ゼネラル・エレクトリック・カンパニイ Variable nozzle in turbine engine, and related method
RU2767250C1 (en) * 2020-12-14 2022-03-17 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" Adjustable inlet guiding apparatus of the compressor of a gas turbine engine

Also Published As

Publication number Publication date
JPS5624772B2 (en) 1981-06-08

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